ERJ 190 GF – Test Copy – Aviator-Training ONLINE

1. Question

In addition to Ground Spoilers, Speed brakes and Flaps/Slats, the SECONDARY Flight Controls System include:

Horizontal stabilizer and Multifunction spoilers
Horizontal stabilizer
Multifunction spoilers

2. Question

In addition to two engine-driven Integrated Drive AC Generators (IDGs) and one APU driven AC Generator (APU GEN), the AC Electrical Power Generating and Distribution System comprises:

One Ram Air Turbine driven AC Generator (RAT) and one AC external power input
One AC external power input
One Ram Air Turbine driven AC Generator (RAT) and two AC external power input

3. Question

In addition to fan cowl and thrust reverser, what parts of engine cowling remain on the pylon when the engine is removed?

Air inlet cowl
Engine core cowl
Engine core cowl and primary exhaust nozzle

4. Question

The airplane has the following ramp interphone panels:

Two Forward and one Aft ramp interphone panels
One Forward, one Center and one Aft ramp interphone panels
One Forward and one Aft ramp interphone panels

5. Question

How many modes of landing gear operation are available to the crew?

There are two: normal hydraulically operated extension and retraction, and mechanical free-fall
There are three: normal hydraulically operated extension and retraction, electrical override, and mechanical free-fall
There are three: normal electro-mechanical operated extension and retraction, electrical override and mechanical free-fall

6. Question

Unscheduled maintenance check(s) have to be performed after the following occurrence(s):

Landing Gear Down Over Speed
Toilet Overservicing
Both answers are correct

7. Question

In addition to anti-ice and air conditioning systems, the pneumatic system supplies controlled bleed air for the purpose of:

Water tank pressurization and engines starting
Engines and APU starting
Water tank pressurization, engines and APU starting

8. Question

The primary source of fuel supply to the engine is:

Electrical Alternating Current pump
Engine-driven pump
Ejector pump

9. Question

In addition to automatic pitch and roll guidance to the elevator and aileron servos, what automatic guidance does the autopilot suppy?

Nothing
Both answers are correct
Automatic yaw guidance to the rudder servo (only for aircraft with Autoland Function)

10. Question

How many remote terminal ports are available on ERJ 190?

Three
Four
Five

11. Question

Please choose the correct continuation: “Thrust reverser is…

… electrically actuated and electronically controlled"
… hydraulically actuated and electrically controlled"
… mechanically actuated and electrically controlled"

12. Question

In addition to the pilot and co-pilot seats, the cockpit seats comprise:

Observer seat
Nothing
Flight engineer seat

13. Question

Which Flight Attendant Panel provides water tank quantity indication?

Forward
Aft
Both

14. Question

In addition to bleed air for the aircraft systems, the Auxiliary Power Unit (APU) supplies:

Electrical power
Electrical and hydraulic power
Hydraulic power

15. Question

In addition to each engine oil tank sight glass, the engine oil quantity information is provided by:

Engine Instrument and Crew Alerting System (EICAS) in the cockpit
Nothing
Multi function Display (MFD) in the cockpit

16. Question

The service light system provides general illumination to the service compartments:

Middle hydraulic compartment
Both answers are correct
Forward, Middle and Aft avionics compartments

17. Question

How many Air Data Smart Probes (ADSP) and Total Air Temperature (TAT) probes does the Air Data System comprise?

Two ADSP and two TAT probes
Two ADSP and four TAT probes
Four ADSP and two TAT probes

18. Question

In addition to elevators, the Fly-by-Wire technology runs the PRIMARY flight controls:

Ailerons and Rudder
Multifunction spoilers, and Rudder
Multifunction spoilers, Horizontal stabilizer and Rudder

19. Question

In addition to stop the fuel flow to the engine, the engine emergency shutdown system:

Stops the flow of fluids and air from the engine to the aircraft systems
Isolates the engine side of the hydraulic system from the airframe hydraulic system
Does nothing

20. Question

In addition to wing, engine intakes, windshields, doors, pitot and static sensors and water lines, the ice and rain protection system prevents ice formation on:

Ice detectors
Stabilizers and ice detectors
Nothing

21. Question

Unscheduled servicing includes:

Aircraft cleaning
Gas replenishing
Cold weather maintenance

22. Question

In addition to two nickel cadmium batteries, the Direct Current Electrical Power Generating and Distribution System comprises:

Nothing
One DC external power input
Two DC external power input

23. Question

How many flight attendant panels are installed on the aircraft?

Two in the forward and one in the aft area of the passenger cabin
One in the forward and one in the aft area of the passenger cabin
One in the forward, one in the middle and one in the aft area of the passenger cabin

24. Question

The wing main structure is made…

… of aluminum alloy and has three spars
… of aluminum alloy a has two spars
… of aluminum alloy with the use of composite and has three spars

25. Question

What is the primary source of hydraulic power of each of hydraulic systems of the airplane?

Engine Driven Pumps – for Systems #1 and #2, AC Electric Motor-Driven Pumps – for Systems #3 and #4
Engine Driven Pumps – for Systems #1 and #2, AC Electric Motor-Driven Pump – for System #3
Engine Driven Pump – for System #1, AC Electric Motor-Driven Pumps – for Systems #2 and #3

26. Question

The Emergency Lights System provides an indication on:

Engine Instrument and Crew Alerting System (EICAS) display and Multi function Display (MFD) number 2
Engine Instrument and Crew Alerting System (EICAS) display
Both Multi function Displays (MFD)

27. Question

How many fire extinguishing bottles are installed in engine fire extinguishing system?

Two fire extinguishing bottles for fire zone of each engine (four in total)
One fire extinguishing bottle for fire zone of each engine (two in total)
Two fire extinguishing bottles for fire zones of both engines (two in total)

28. Question

The Inertial Reference Units are…

… installed in the FWD avionics compartment and intended to indicate current position of the airplane relative to the ground
… installed in the middle avionics compartment and intended to indicate current position of the airplane relative to the ground
… installed in the FWD avionics compartment and intended to sense and compute linear accelerations and angular turning rates about the airplane’s axes

29. Question

How many oxygen sources are available for flight crew?

Two
Three
One

30. Question

What engine core compressor stages have bleed ports for customer bleed air connection?

Stages numer 5 and 10
Stages numer 5 and 9
Stages numer 4, 5 and 9

31. Question

In addition to Tail Strike Avoidance and Mach Trim compensation, the Flight Control Module provides High Level Functions as feature of ERJ 190-100/200:

Elevator Autoconfiguration function
Automatic Trim Compensation and Elevator Autoconfiguration function
Angle-Of-Attack limiting

32. Question

How many Digital Voice Data Recorders (DVDR) and Quick Access Recorders (QAR) does the Recorders System include?

One DVDR and one QAR
Two DVDRs and one QAR
Two DVDRs and two QARs

ERJ 190 GF – Test Copy

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